Title :
Design and analysis of optimal controller for fuzzy systems with input constraint
Author :
Park, Yonmook ; Tahk, Min-Jea ; Bang, Hyochoong
Author_Institution :
Dept. of Mech. Eng., Korea Adv. Inst. of Sci. & Technol., Daejeon, South Korea
Abstract :
In this paper, we present a design method of the optimal and robust controller subject to the constraint on control inputs for continuous-time Takagi-Sugeno (TS) fuzzy systems. In order to establish this design method, we consider an optimal and robust control problem for nonlinear dynamic systems. For this problem, we present an analytic way which can provide the optimal controller for nonlinear dynamic systems by the dynamic programming approach and the inverse optimal approach. Moreover, we analyze the robustness property of the proposed optimal controller with respect to a class of input uncertainties by the passivity approach. Then, based on the theoretical results presented in this paper, we formulate the design problem of the optimal and robust controller with input constraint for continuous-time TS fuzzy systems as the semidefinite programming problem, and find the controller by solving it. The usefulness of the proposed approach is illustrated by considering the three-axis attitude stabilization problem of rigid spacecraft.
Keywords :
continuous time systems; control system analysis; control system synthesis; dynamic programming; fuzzy control; fuzzy systems; nonlinear control systems; nonlinear dynamical systems; optimal control; robust control; Takagi-Sugeno fuzzy systems; dynamic programming; inverse optimal approach; nonlinear dynamic systems; optimal control; rigid spacecraft; robust control; semidefinite programming problem; three-axis attitude stabilization; Control system analysis; Control systems; Design methodology; Dynamic programming; Fuzzy systems; Nonlinear control systems; Optimal control; Robust control; Takagi-Sugeno model; Uncertainty; Optimal and robust control; Takagi–Sugeno (TS) fuzzy system; passivity approach; semidefinite programming problem; spacecraft attitude control;
Journal_Title :
Fuzzy Systems, IEEE Transactions on
DOI :
10.1109/TFUZZ.2004.836089